As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN IS DENTED AROUND RIVETS T FRAMES 70 - 72; STRINGER 22R. RE-EVALUATED THE AREA & FOUND TO BE OUT OF LIMITS IAW SRM 53-17-12 & SRM 53-10-00. REMOVED DAMAGED AREA IAW SRM 53-10-12. FABRICATED THE FILLER & DOUBLER REPAIR IAW SRM 53-10-12. ALODINED & PRIMED IAW SRM 53-23-10. INSTALLED DOUBLER REPAIR IAW SRM 51-40-21.